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Frontiers in Energy

ISSN 2095-1701

ISSN 2095-1698(Online)

CN 11-6017/TK

Postal Subscription Code 80-972

2018 Impact Factor: 1.701

Front. Energy    2019, Vol. 13 Issue (4) : 764-769    https://doi.org/10.1007/s11708-016-0449-z
RESEARCH ARTICLE
Structural optimal design of a swing vane compressor
Junjie MA(), Xiang CHEN, Zongchang QU
School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, China
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Abstract

In this paper, a novel swing vane rotary compressor (SVC) was introduced, which had significant advantages—simple mechanism, reduced frictional loss, reliable operation, and a comparatively higher compression ratio. Based on the swing vane compressor geometry model, thermodynamic model and kinetic model, the mathematical model of optimum design was established, and further theoretical and experimental studies were conducted. The length of the cylinder, radius of the rotor and cylinder were defined as design variables and the reciprocal of EER as objective function. The complex optimization method was adopted to study the structure of the swing vane compressor. The theoretical model could provide an effective method for predicting compressor performance, which would also contribute to structural optimization of the SVC. The study shows that the friction loss of the compressor are greatly reduced by optimized design in a given initial value, and the EER increased by 8.55%.

Keywords swing vane compressor      simulation      optimization design     
Corresponding Author(s): Junjie MA   
Just Accepted Date: 14 November 2016   Online First Date: 08 February 2017    Issue Date: 26 December 2019
 Cite this article:   
Junjie MA,Xiang CHEN,Zongchang QU. Structural optimal design of a swing vane compressor[J]. Front. Energy, 2019, 13(4): 764-769.
 URL:  
https://academic.hep.com.cn/fie/EN/10.1007/s11708-016-0449-z
https://academic.hep.com.cn/fie/EN/Y2019/V13/I4/764
Fig.1  Structure of SVC
Fig.2  Working process of SVC
Fig.3  The description of the complex method
VariablesL-limit/mmU-limit/mm
Rcy4267
Rpis3958
H1431
Tab.1  Scope of design variables
Fig.4  Compressor chamber pressure
Fig.5  Compressor chamber pressure
Fig.6  Change of chamber temperature
Fig.7  Change of chamber mass
ParametersValues
Working volume/cm2377.2
Revolving speed/(r·min-1)2500
Suction pressure/bar2.8
Discharge pressure/bar18.048
Initial values(Rcy, Rpis, H)[47.3, 41.7, 24.1]
Initial EER1.9476
Optimization values(Rcy, Rpis, H)(64.6, 55.9, 29.6)
Optimized EER2.1132
Tab.2  Values of parameters
Fig.8  Change of objective function
Fig.9  Change of error vector
Fig.10  Change of vector |fmax?fmin|
Fig.11  Change of EER
Avalve flow area /m2
bthickness of vane /m
Cddischarge coefficient
eeccentric distance /m
Fforce /N
Hheight of rotor /m
Llength /m
Lffrictional loss /W
mmass of fluid /kg
nrotational speed of compressor /(r·min-1)
ppressure /Pa
Qheat transfer rate /W
Q0cooling capacity /W
Rradius /m
Ttemperature /K
Uvelocity / (m·s-1)
Vvolume /m3
vspecific volume /(m3·kg-1)
Wiindicate work /J
dclearance /m
qdrive angle /rad
εbearing eccentric ratio
ηkinetic friction coefficient
μdynamic viscosity of lubricant /(pa.s)
ωangular velocity /(rad·s-1)
Subscripts:
isuction conditions
odischarge conditions
ccylinder chamber conditions
bebearing
clradial clearance
cycylinder
ececcentric
efat end face
vvane
rin radial direction
τin tangential direction
vsat vane side
vtat vane tip
  
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